首页> 外文会议>56th International Astronautical Congress 2005 vol.9 >ORPHEUS PROJECT: A STUDY PROPOSAL FOR A MARS ISRU PLANT
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ORPHEUS PROJECT: A STUDY PROPOSAL FOR A MARS ISRU PLANT

机译:ORPHEUS项目:火星岛植物的研究建议

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Space exploration has always been drastically constrained by the launchable mass, this is extremely important asrna spacecraft needs to be returned to Earth because of the way back-propellant.rnThe growing interest for Mars exploration and its eventual manned colonization impose to test new technologiesrnand try different approaches to the problem. A possible solution is to install an In Situ Resource Utilization,rnISRU, platform on the surface of Mars, able to produce the needed propellant using the resources available in thernMartian environment.rnOrpheus Project is a technological demonstrator whose purpose is to show the advantages of an In SiturnPropellant Production, ISPP, instead of carrying all the extra propellant from Earth. The main task of this projectrnis to show that the weight of the propellant produced by the ISPP plant is greater than the one of the producingrnsystem itself.rnTwo different scenarios have been investigated: A Small Size Mission (SSM), the technological demonstrator,rnmore conservative, with a contained launch mass, able to bring back to Earth 3 kg producing C_2H_4/O_2 in situ. ArnLarge size Mission (LSM), the full scale mission, more futuristic, designed to show that is possible to producernenough propellant to launch a manned module (about 2250 Kg) from a Martian human base.rnThis paper mainly focuses on the first mission, the technological demonstrator, its design and its feasibility.
机译:太空探索历来受到可发射物质的极大限制,这是非常重要的,因为反向推进方式,需要将Asrna航天器返回地球。rn对于火星探索及其最终的有人为殖民化的兴趣日益浓厚,这就要求测试新技术并尝试不同解决问题的方法。一种可能的解决方案是在火星表面安装Insitu Resource Utilization,rnISRU平台,该平台能够使用rnMartian环境中可用的资源来生产所需的推进剂。在“ Siturn推进剂生产”中,ISPP而不是从地球上带走所有多余的推进剂。该项目的主要任务是表明ISPP工厂生产的推进剂的重量大于生产系统本身的重量。研究了两种不同的情况:小型任务(SSM),技术演示者,更为保守,其发射质量得以控制,能够将3千克原位带回地球的C_2H_4 / O_2。 ArnLarge size Mission(LSM)是一种全面的任务,更具未来性,旨在表明足够的推进剂可以从火星人基地发射载人模块(约2250 Kg)。rn本文主要关注第一个任务,即技术演示器,其设计和可行性。

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